SE0002504L - Sätt och anordning för att förhindra att inkapslade explosivämnen bringas att explodera av en utvändig brand - Google Patents
Sätt och anordning för att förhindra att inkapslade explosivämnen bringas att explodera av en utvändig brandInfo
- Publication number
- SE0002504L SE0002504L SE0002504A SE0002504A SE0002504L SE 0002504 L SE0002504 L SE 0002504L SE 0002504 A SE0002504 A SE 0002504A SE 0002504 A SE0002504 A SE 0002504A SE 0002504 L SE0002504 L SE 0002504L
- Authority
- SE
- Sweden
- Prior art keywords
- exploding
- preventing
- external fire
- methods
- explosives
- Prior art date
Links
- 239000002360 explosive Substances 0.000 title abstract 4
- 229910001285 shape-memory alloy Inorganic materials 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
- F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Fire-Detection Mechanisms (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Air Bags (AREA)
- Disintegrating Or Milling (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0002504A SE519561C2 (sv) | 2000-07-03 | 2000-07-03 | Anordning vid raketmotorer för att förhindra att raketmotor bringas att explodera vid utvändig brand |
EP01941402A EP1297303B1 (en) | 2000-07-03 | 2001-06-19 | Arrangement for preventing encased explosives being caused to explode by an external fire |
US10/312,511 US7051511B2 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
PCT/SE2001/001370 WO2002003019A1 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
AU2001274759A AU2001274759A1 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explodeby an external fire |
IL15363001A IL153630A0 (en) | 2000-07-03 | 2001-06-19 | Method and arrangement for preventing encased explosives being caused to explode by an external fire |
AT01941402T ATE314622T1 (de) | 2000-07-03 | 2001-06-19 | Vorrichtung zur verhinderung der explosion umhüllter sprengstoffe während eines externen feuers. |
DE60116309T DE60116309T2 (de) | 2000-07-03 | 2001-06-19 | Vorrichtung zur Verhinderung der Explosion umhüllter Sprengstoffe während eines externen Feuers. |
IL153630A IL153630A (en) | 2000-07-03 | 2002-12-24 | Arrangement of a rocket engine to prevent explosive material from exploding from high outside temperature |
NO20030006A NO327421B1 (no) | 2000-07-03 | 2003-01-02 | Fremgangsmate og anordning for a forhindre at innkapslede eksplosiver pavirkes til a eksplodere ved en ekstern brann |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0002504A SE519561C2 (sv) | 2000-07-03 | 2000-07-03 | Anordning vid raketmotorer för att förhindra att raketmotor bringas att explodera vid utvändig brand |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0002504D0 SE0002504D0 (sv) | 2000-07-03 |
SE0002504L true SE0002504L (sv) | 2002-01-04 |
SE519561C2 SE519561C2 (sv) | 2003-03-11 |
Family
ID=20280352
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0002504A SE519561C2 (sv) | 2000-07-03 | 2000-07-03 | Anordning vid raketmotorer för att förhindra att raketmotor bringas att explodera vid utvändig brand |
Country Status (9)
Country | Link |
---|---|
US (1) | US7051511B2 (sv) |
EP (1) | EP1297303B1 (sv) |
AT (1) | ATE314622T1 (sv) |
AU (1) | AU2001274759A1 (sv) |
DE (1) | DE60116309T2 (sv) |
IL (2) | IL153630A0 (sv) |
NO (1) | NO327421B1 (sv) |
SE (1) | SE519561C2 (sv) |
WO (1) | WO2002003019A1 (sv) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2391899A (en) * | 2002-08-12 | 2004-02-18 | Qinetiq Ltd | Shape memory alloy connector and an overwound munition casing |
US8082846B2 (en) | 2002-08-12 | 2011-12-27 | Qinetiq Limited | Temperature responsive safety devices for munitions |
SE0300834L (sv) * | 2003-03-26 | 2004-07-20 | Saab Ab | Verkansdel |
US7373885B2 (en) * | 2005-10-28 | 2008-05-20 | Lockheed Martin Corporation | Device for venting a container housing an energetic material and method of using same |
US7469538B2 (en) * | 2005-10-28 | 2008-12-30 | Searete Llc | Self assembling/quick assembly structure using shape memory alloy materials |
US8720722B2 (en) * | 2005-12-15 | 2014-05-13 | Cornerstone Research Group, Inc. | Venting mechanism for containers |
WO2008127806A1 (en) * | 2007-03-07 | 2008-10-23 | Cornestone Research Group, Inc. | Venting mechanisms for containers |
ATE425430T1 (de) * | 2006-01-13 | 2009-03-15 | Saab Ab | Sicherheitsmechanismus für waffen mit vorgeladenen geschossen. |
EP1808668B1 (en) * | 2006-01-17 | 2011-04-27 | Saab Ab | An internal pressure relieving device for anti-armour ammunition |
US7762195B2 (en) * | 2007-05-14 | 2010-07-27 | Aerojet - General Corporation | Slow cook off rocket igniter |
GB0714440D0 (en) * | 2007-07-25 | 2007-10-17 | Qinetiq Ltd | Rupturing device |
FR2931874B1 (fr) * | 2008-05-29 | 2010-06-25 | Snecma | Dispositif de blocage axial d'un palier de guidage d'arbre dans une turbomachine. |
US7743752B2 (en) * | 2008-07-18 | 2010-06-29 | Ford Global Technologies, Llc | System and method for improving fuel vapor purging for an engine having a compressor |
EP2335011B1 (en) * | 2008-10-10 | 2017-03-29 | Saab AB | A cartridge case and a round comprising such a cartridge case |
DK2335010T3 (en) * | 2008-10-10 | 2017-03-27 | Saab Ab | CARTRIDGE AND A CHARGE INCLUDING SUCH A CARTRIDGE |
FR2948186B1 (fr) * | 2009-07-17 | 2015-02-20 | Tda Armements Sas | Munition comprenant des moyens pour neutraliser son chargement explosif |
US8578855B2 (en) | 2009-08-21 | 2013-11-12 | General Dynamics Armament And Technical Products, Inc. | Rocket motor tube with safety features |
US8925463B1 (en) * | 2009-09-03 | 2015-01-06 | Kms Consulting, Llc | Pressure relief system for gun fired cannon cartridges |
US8230682B1 (en) | 2009-09-24 | 2012-07-31 | The United States Of America As Represented By The Secretary Of The Navy | Thermally activated initiator assembly |
US9482185B1 (en) * | 2014-02-20 | 2016-11-01 | The United States of America as Reprented by the Secretary of the Navy | Thermal rocket initiator mechanism and rocket system incorporating same |
ES2703550T3 (es) * | 2014-04-11 | 2019-03-11 | Saab Ab | Disposición para bloquear condiciones de armado |
DE102014013316B4 (de) | 2014-09-08 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Behältnis zur Aufbewahrung eines Explosivstoffs |
US10113846B2 (en) | 2016-07-07 | 2018-10-30 | General Dynamics Ordnance and Tactical Systems-Canada, Inc. | Systems and methods for reducing munition sensitivity |
US10801822B2 (en) * | 2018-06-29 | 2020-10-13 | Goodrich Corporation | Variable stand-off assembly |
IL260886B (en) * | 2018-07-30 | 2021-04-29 | Rafael Advanced Defense Systems Ltd | Rocket armament that can be launched from a tubular launcher with non-ignition security outside the launcher and engine separation in flight |
CN110985237A (zh) * | 2019-11-13 | 2020-04-10 | 上海新力动力设备研究所 | 基于记忆合金技术高温下失效的连接固定装置及应用方法 |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR540418A (fr) | 1919-01-13 | 1922-07-11 | Dispositif de contrôle pour moteurs à combustion interne | |
US3776466A (en) * | 1973-01-19 | 1973-12-04 | W Ray | Polyurethane foam insert for overexpanded rocket engine nozzles to prevent start transient sideloads |
US4022129A (en) * | 1976-01-16 | 1977-05-10 | The United States Of America As Represented By The Secretary Of The Air Force | Nozzle ejection system |
US4084512A (en) | 1976-10-18 | 1978-04-18 | The United States Of America As Represented By The Secretary Of The Navy | Pressure relief construction for controlled combustion of ordnance items |
US4272956A (en) * | 1979-01-22 | 1981-06-16 | Thiokol Corporation | Time delay device for deployable rocket nozzle skirts |
FR2503794B1 (fr) * | 1981-04-13 | 1986-04-25 | Europ Propulsion | Chambre de combustion de propulseur-fusee a divergent multiple |
US4458482A (en) | 1982-05-17 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Rocket motor |
US4442666A (en) | 1982-10-21 | 1984-04-17 | The United States Of America As Represented By The Secretary Of The Navy | Fuel fire resistant motor |
US4477024A (en) * | 1983-04-05 | 1984-10-16 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon rocket motor exit cone reinforcement |
US5540949A (en) * | 1986-04-24 | 1996-07-30 | The United States Of America As Represented By The Secretary Of The Air Force | Method for cutting threads in a carbon-carbon structure |
JPH02216398A (ja) * | 1989-02-17 | 1990-08-29 | Nissan Motor Co Ltd | 結合体の分離装置 |
US5036658A (en) * | 1990-03-05 | 1991-08-06 | The United States Of America As Represented By The Secretary Of The Army | Pressure relief device for solid propellant motors subjected to high external temperatures |
US5311820A (en) * | 1991-01-17 | 1994-05-17 | Thiokol Corporation | Method and apparatus for providing an insensitive munition |
US5735114A (en) * | 1991-08-15 | 1998-04-07 | Thiokol Corporation | Thermostatic bimetallic retaining ring for use in rocket motor assembly |
FR2683312B1 (fr) * | 1991-10-31 | 1994-01-28 | Etat Francais Delegue Armement | Dispositif de securite de fonctionnement pour engin explosif et/ou propulsif soumis a une variation de temperature. |
FR2686410A1 (fr) * | 1992-01-22 | 1993-07-23 | France Etat Armement | Dispositif assurant le deconfinement d'une charge contenant un explosif par mise en óoeuvre d'un element deformable en materiau a memoire de forme. |
FR2699663B1 (fr) * | 1992-12-18 | 1995-02-24 | Giat Ind Sa | Dispositif d'initiation pour un système pyrotechnique. |
US5394803A (en) * | 1994-02-14 | 1995-03-07 | Bel Electronics, Inc. | Joint construction between military rocket motor and warhead and releasable by melting of fusible eutectic wedging ring for operating flexible locking fingers |
SE508650C2 (sv) | 1994-03-10 | 1998-10-26 | Bofors Ab | Sätt att vid patronerad stridsammunition minska skadeverkan i omgivningen vid extrema tryckstegringar i ammunitionens drivladdningar samt patronhylsa för stridsammunition |
FR2742221B1 (fr) * | 1995-12-12 | 1998-02-27 | Soc D Ateliers Mecaniques De P | Dispositif de deconfinement pour munition |
US5779151A (en) * | 1996-05-28 | 1998-07-14 | Regents Of The University Of California | Stepped nozzle |
FR2754566B1 (fr) * | 1996-10-11 | 1999-02-05 | Europ Propulsion | Tuyere de moteur-fusee a inserts ejectables |
US5792981A (en) * | 1996-10-28 | 1998-08-11 | Thiokol Corporation | Gun-launched rocket |
US6321656B1 (en) * | 2000-03-22 | 2001-11-27 | The United States Of America As Represented By The Secretary Of The Navy | Thermally actuated release mechanism |
JP3940893B2 (ja) * | 2001-12-14 | 2007-07-04 | 石川島播磨重工業株式会社 | ロケットとペイロードとのクランプバンド |
US6752085B2 (en) * | 2002-05-06 | 2004-06-22 | Lockheed Martin Corporation | Method and apparatus for releasably attaching a closure plate to a casing |
-
2000
- 2000-07-03 SE SE0002504A patent/SE519561C2/sv not_active IP Right Cessation
-
2001
- 2001-06-19 US US10/312,511 patent/US7051511B2/en not_active Expired - Fee Related
- 2001-06-19 EP EP01941402A patent/EP1297303B1/en not_active Expired - Lifetime
- 2001-06-19 DE DE60116309T patent/DE60116309T2/de not_active Expired - Lifetime
- 2001-06-19 AT AT01941402T patent/ATE314622T1/de not_active IP Right Cessation
- 2001-06-19 WO PCT/SE2001/001370 patent/WO2002003019A1/en active IP Right Grant
- 2001-06-19 IL IL15363001A patent/IL153630A0/xx active IP Right Grant
- 2001-06-19 AU AU2001274759A patent/AU2001274759A1/en not_active Abandoned
-
2002
- 2002-12-24 IL IL153630A patent/IL153630A/en not_active IP Right Cessation
-
2003
- 2003-01-02 NO NO20030006A patent/NO327421B1/no not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE60116309T2 (de) | 2006-08-24 |
IL153630A0 (en) | 2003-07-06 |
US7051511B2 (en) | 2006-05-30 |
DE60116309D1 (de) | 2006-02-02 |
AU2001274759A1 (en) | 2002-01-14 |
US20040244358A1 (en) | 2004-12-09 |
NO327421B1 (no) | 2009-06-29 |
EP1297303A1 (en) | 2003-04-02 |
SE519561C2 (sv) | 2003-03-11 |
WO2002003019A1 (en) | 2002-01-10 |
NO20030006D0 (no) | 2003-01-02 |
SE0002504D0 (sv) | 2000-07-03 |
ATE314622T1 (de) | 2006-01-15 |
IL153630A (en) | 2006-10-31 |
NO20030006L (no) | 2003-02-28 |
EP1297303B1 (en) | 2005-12-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |